> ## Documentation Index
> Fetch the complete documentation index at: https://docs.ntop.com/llms.txt
> Use this file to discover all available pages before exploring further.

# F-16 R6: fair airfoils and finite trailing edges

> AI context for F-16 R6: fair airfoils and finite trailing edges. Not linked in navigation.

> This page is for AI assistant context only. To use this package, visit [community.ntop.com](https://community.ntop.com/#/detail/f16-fair-airfoils-r6).

> **Community submission — not verified by nTop.** This package was submitted by an outside community member and has not been reviewed or verified by nTop. Treat its accuracy, safety, and compatibility claims with appropriate caution.

## Summary

Inspect the R6 aircraft appearance study with fair airfoils, revised aft-fuselage guides, and finite trailing edges.

## Package Details

| Field | Value |
| - | - |
| **ID** | `f16-fair-airfoils-r6` |
| **Type** | Notebook |
| **Author** | nTop |
| **Version** | 0.1.0 |
| **nTop Version** | 6.0 |
| **Domain** | Aerospace |
| **Application** | Geometry |
| **Complexity** | Advanced |
| **Tags** | `notebook-api`, `parametric`, `modeling`, `geometry`, `ai-assisted` |
| **License** | MIT |
| **Verified** | No |

***

**Built with Astra.**

Inspect the R6 aircraft appearance study with fair airfoils, revised aft-fuselage guides, and finite trailing edges.

<img src="https://mintlify.s3.us-west-1.amazonaws.com/ntopology/community/packages/bradrothenberg/cover.png" alt="F-16 R6: fair airfoils and finite trailing edges" />

The saved graph preserves R6 geometry and editable controls. Earlier cross-CAD comparisons use R3 and must not be treated as R6 measurements. Replay does not repeat the original fitting process.

## Installation and use

1. Download the package files and keep them together.
2. Open `f16-fair-airfoils-r6.ntop` in the matching licensed nTop build.
3. Save a working copy before editing. Expand the relevant section and change one control at a time.
4. Inspect the rebuilt bodies and block states before accepting the changed model.

Recorded native build: **6.0.0-rc 42594**. The catalogue version field cannot encode the custom build number. Public release compatibility has not been re-tested. The application and license are not included.

## Inputs and outputs

| Direction | Contents |
| - | - |
| Input | Saved native guide and airfoil controls |
| Output | Editable aircraft exterior and component geometry |

Named scalar controls include `Wingspan`, `Scale factor`, `Fuselage width multiplier`, `Fuselage height multiplier`, `Canopy height multiplier`, `Wing thickness multiplier`, `Trailing edge thickness at 32 ft`, `Normalized trailing edge thickness`, `Wing tip chord multiplier`, `Wing tip twist slope`, `Tail thickness multiplier`, `Fin thickness multiplier`. Some are computed values; inspect their upstream construction before changing them.

## Files

* [f16-fair-airfoils-r6.ntop](f16-fair-airfoils-r6.ntop)

## Evidence and source

Publication checks are offline: native-container round trips, export-path changes, collapsed presentation, dependency inspection, and binary payload preservation. These checks do not constitute new native execution. See [publication-checks.json](publication-checks.json).

The [source, usage notes, and recorded report](https://github.com/bradrothenberg/ntop-api-share/tree/92f13bc0a873aacba62526ee43e9e6895ef051f8/demos/f16) retain the original construction and verification scope. Download the public source checkout to view reports with their local assets.

## License

MIT. See [LICENSE](LICENSE). This license covers the original example models, saved recipes, and supporting material in this package.

***

## Source

[https://community.ntop.com/#/detail/f16-fair-airfoils-r6](https://community.ntop.com/#/detail/f16-fair-airfoils-r6)

## Download

[Download f16-fair-airfoils-r6.ntop](https://github.com/nTopology/Utilities-community/releases/download/f16-fair-airfoils-r6-v0.1.0/f16-fair-airfoils-r6.ntop)


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